N145FE
Service difficulty reports · 45
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N145FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N145FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202610111553Floorboard · puncturedMAIN DECK FLOOR PANEL 252EFF HAS PUNCTURE DAMAGE. DB05 FABRICATED FLOORBOARD 252EFF (MPN: 146T5869-155) REF BOEING DWG 146T5869-155 AND FEDEX DWG SR67-53-009. SEE JPF FOR WORK STEPS PERFORMED. THIS IS A MAJOR REPAIR.SDR FDEA202610031471Skin · damagedR/H WING, INBD AFT FLAP LOWER SURFCE HAS IMPACT DAMAGE LOCATED APPOX. 42" FROMINBD EDGE AND APPROX. 6" FROM AFT EDGE. REPAIRED R/H WING INBD AFT FLAP TRAILING EDGE WEDGE LWR SURFACE APPROX. 42" FROM INBD EDGE AND APPROX. 6" FROM AFT EDGE AN AREA OF .3 X .SDR FDEA202610021470Skin · dentedLEFT WING OUTBOARD TRAILING EDGE FLAP HAS MULTIPLE AREAS OF DAMAGE. SKIN REPAIR IS BEING DONE WITH TWO SEPERATE REPAIRS, THIS ITEM IS TO DOCUMENT THE SECOND REPAIR. REPAIRED DAMAGED TOPSKIN ON LWR SURFACE OF L/H WING O/B FLAP TRAILING EDGE WEDGE AREA OF SDR FDEA202610021469Skin · dentedLEFT WING OUTBOARD TRAILING EDGE FLAP, UNDERSIDE OF TRAILING EDGE WEDGE, INSIDE OF OUTBOARD FLAP FAIRING, HAS MULTIPLE AREAS OF DELAMINATION. MARKED WITH TAPE. REPAIRED DAMAGED TOPSKIN ON LWR SURFACE OF L/H WING O/B FLAP TRAILING EDGE WEDGE AREA OF 9 X 5 SDR FDEA202507081143Sensor · failedEMERGENCY DECLARED FOR LE SLAT ASYM INDICATION. AT APPROXIMATELY 1500 AFE AND 160 KNOTS, WE WERE AT FLAPS 25 WITH NORMAL INDICATIONS. WHEN SELECTING FLAPS 30, THE LE SLAT ASYM EICAS MESSAGE APPEARED ALONG WITH THE LEADING EDGE DISCRETE LIGHT. WENT AROUND SDR FDEA202409251369Floor Panel · dentedMAIN DECK CARGO, FLOOR PANEL 241WFF WITH DENTS MDC,FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 SHEET 2 REV.90 AUG 15/2024SDR FDEA202409251368Floor Panel · crackedMAIN DECK CARGO, FLOOR PANEL 242VFF WITH PUNCTURES MDC , FLOOR PANEL 242VFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV: 90 AUG 15/2024SDR FDEA202409251367Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222AFF. MDC FLOOR PANEL 222AFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV: 90 AUG 15/2024SDR FDEA202409251366Floor Panel · crackedMAIN DECK CARGO, FLOOR PANEL 241AGF WITH PUNCTURES MAIN DECK CARGO, FLOOR PANEL 241AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15/2024SDR FDEA202409251365Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 221DFF. MDC FLOOR PANEL 221DFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV: 90 AUG 15/2024SDR FDEA202409251364Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 221CFF. MDC FLOOR PANEL 221 CFF MDC WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV: 90 AUG 15/2024SDR FDEA202409251363Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222BFF. MDC FLOOR PANEL 222BFF,MDC WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV: 90 AUG 15/2024SDR FDEA202409251362Floor Panel · dentedMAIN DECK CARGO, FLOOR PANEL 242SFF WITH DENTS MDC FLOOR PANEL 242SFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG.201 SHEET 2 REV.90 AUG 15/2024SDR FDEA202404240294Washer · missingMDIS 145 32-41 5927 24APR24 13:26 MTY FACT ON WALKAROUND RH NOSE TIRE FOUND AXLE NUT NEAR TO FLUSH WITH THE END OF THE AXLE. MXALERT 20-0126. AFTER THE REMOVAL OF THE RH WHEEL TANG WASHER IS MISSING. PART 24APR24 13:26 MTY IDENTIFIED PARTSSDR FDEA202404240285Washer · missingON WALKAROUND RH NOSE TIRE FOUND AXLE NUT NEAR TO FLUSH WITH THE END OF THE AXLE. MXALERT 20-0126. AFTER THE REMOVAL OF THE RH WHEEL TANG WASHER IS MISSING. TANG WASHER INSTALLED ON RH NLG WHEEL IAW AMM.A/C OK FOR SVC.SDR FDEA202202280375Skin · delaminatedFOUND RT WING OUTBOARD FLAP DELAMINATED ON TAILING EDGE 6 INCHES INBOARD OF OTBD FLAP CANOE. REMOVED DAMAGE MATERIAL CLEANED AND PREPPED AREA FOR BONDING FOR RT WING OTBD FLAP TE 6 INCHES INB OF OTBD CANOE.SDR FDEA202104180950Evas Unit · failedWHILE COMPLYING WITH EO H-2560-E0324416, REV G POS. P2. FOUND LT EVAS BATTERY TEST BUTTON REMAINED DEPRESSED AND UNABLE TO TEST. REMOVED AND REPLACED LT EVAS REF AMM 25-99-99-4. OPS CHECKED GOOD.SDR FDEA202010252650Beam · crackedRIGHT WING FIXED LEADING EDGE OSS 679 NOSE BEAM WEB CRACKED. REPAIRED RIGHT WING FIXED LEADING EDGE OSS 679 NOSE BEAM WEB, IAW B767 SRM 57-41-13-2R REPAIR 3.SDR FDEA202010252649Skin · puncturedLT WING, NR 1 SPOILER UPPER SURFACE IS PUNCTURED APPROXIMATELY 2" FROM OUTBOARD EDGE. EVALUATED REMOVED SEAL TO FOM. PERFORMED REPAIR, IAW B767 SRM 57-70-01-2R-1 FIG 201, SRM 57-70-01-0I-1 FIG 1, SRM 51-70-04-0G PARA 4 AND FIG 14, SRM 51-40-04-0G, SRM 51-40SDR FDEA202010242644Skin · gougedLEFT WING NR 5 SLAT TRAILING WEDGE LOWER SKIN GOUGED. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE, IAW B767 SRM 57-43-02-2R AND 51-70-10.SDR FDEA202010242643Skin · gougedRIGHT WING NR 9 SLAT TRAILING EDGE WEDGE LOWER SKIN IS GOUGED. REPAIRED NR 9 SLAT TRAILING WEDGE, IAW B767 SRM 57-43-02-2R AND 51-70-10.SDR FDEA202010242639Skin · scratchedRT INBOARD ELEVATOR TRAILING EDGE HAS A SCRATCH 2" FRIM INBOARD EDGE AND 9.25" FROM TRAILING EDGE. REPAIRED SCRATCH ON RIGHT HAND INBOARD ELEVATOR TRAILING EDGE AND RESTORED PAINT FINISH, IAW B767 SRM 51-70-17 PARA 4G AND FEDEX EA H-5520-T0357497-P1. STABILISDR FDEA202010242638Skin · puncturedSMALL PUNCTURE ON TOP SURFACE OF ELEVATOR APPROXIMATELY 20.5 IN. FROM INBOARD EDGE AND APPROXIMATELY 11.25 IN. FROM ELEVATOR TRAILING EDGE REPAIRED PUNCTURE ON TOP SURFACE OF ELEVATOR AND RESTORED PAINT FINISH, IAW B767 SRM 55-20-01 FIG 201 AND SRM 51-70-17-SDR FDEA202010242636Floor Panel · damagedCABIN FLOOR PANEL 242GFF IS PUNCTURED. REPAIRED CABIN FLOOR PANEL 242GFF, IAW B767 SRM 53-00-50-2R PARA 4D.SDR FDEA202010242635Floor Panel · damagedCABIN FLOOR PANEL 241GFF IS PUNCTURED. REPAIRED CABIN FLOOR PANEL 241GFF, IAW B767 SRM 53-00-50-2R PARA 4E.SDR FDEA202010232616Seal Depressor · crackedAFT CARGO DOOR CUT PRESSURE SEAL DEPRESSOR FWD CENTER IS CRACKED. REMOVED AND REPLACED AFT CARGO DOOR FWD CENTER SEAL DEPRESSOR P/N 143T8542-1, IAW B767 SRM 51-40-02, SRM 51-20-01.SDR FDEA202010222605Former · crackedLT WING LEADING EDGE NOSE FORMER AT STA OSS 499 IS CRACKED. REMOVED AND REPLACED NOSE FORMER, PER BAC DWG 114T6161 REV- AND FEDEX EA H-5720- T0357481 P1 WINGS-SECONDARY WING STRCT-LT WING, LEADING EDGE, ANGLE, OSS 499, ALTERNATE FASTENERS.SDR FDEA202010222604Former · crackedRT WING LEADING EDGE NOSE FORMER AT STA OSS 499 IS CRACKED. REMOVED AND REPLACED, PER BAC DWG 114T2161 REV- AND FEDEX EA H-5720-T0357548 P1. WINGS-SECONDARY WING STRCT-RT WING, LEADING EDGE, ANGLE, OSS 499, ALTERNATE FASTENERS.SDR FDEA202010222602Attach Bracket · crackedNR 1 PYLON ATTACH ANGLE CRACKED FWD OF 437BR REPLACED CRACKED BRACKET WITH NEW BRACKET P/N 313T3310-1155, REF BAC DWG 313T2310 REV-, B767 SRM 51-40-02.SDR FDEA202010212591Retainer · crackedAFT CARGO DOOR CUT PRESSURE SEAL RETAINER IS CRACKED AND DENTED. REMOVED AND REPLACED AFT CARGO DOOR PRESSURE SEAL RETAINER BETWEEN STATIONS 1241 AND 1285, IAW B767 SRM 52-30-02-2R, SRM 51-40-02, AMM 52-09-02-4 AND BAC DWG 143T6324 REV-.SDR FDEA202010212588Rib · crackedRT WING LEADING EDGE NOSE RIB AT OSS 441 IS CRACKED. REMOVED AND REPLACED NOSE RIB FORMER, PER H-5720-T0357476 WINGS-SECONDARY STRCT-RT WING, LEADING EDGE, ANGLE, OSS 441, ALTERNATE FASTENERS.AND BAC DWG114T2241 REV.SDR FDEA202010212587Angle · crackedFABRICATE NEW ANGLE P/N 114T2171-3, PER FEDEX EA H-5720-T0357476 P1. FABRICATED NEW ANGLE P/N 114T2171-3, PER FEDEX EA H-5720-T0357476 WINGS-SECONDARY STRCT-RT WING, LEADING EDGE ANGLE, OSS 441, ALTERNATE FASTENERS AND BAC DWG 114T2171 REV A.SDR FDEA202010212586Skin Splice · crackedRT WING LEADING EDGE SKIN SPLICE STRAP IS CRACKED AT STA OSS 514. REMOVED AND REPLACED SKIN SPLICE STRAP, PER B767 SRM 51-40-02 AND BAC DWG 114T2800 REV C.SDR FDEA202010212585Bracket · crackedLT WING LEADING EDGE TORQUE TUBE BRACKET AT STA OSS 514 IS CRACKED. REMOVED AND REPLACED TORQUE TUBE BRACKET, PER BAC DWG 114T2800 REV C AND B767 SRM 51-40-02.SDR FDEA202010212584Bracket · crackedLT WING LEADING EDGE INBOARD SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET, PER BAC DWG 114T1240 REV.SDR FDEA202010212583Bracket · crackedRT WING LEADING EDGE SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET, PER BAC DWG 114T1240 REV AND B767 SRM 51-40-02.SDR FDEA202010212579Bracket · crackedLEFT WING FUEL PANEL, 521QB INTERNAL HOLD OPEN BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET, PER B767 SRM 51-40-02 AND BAC DWG 114T2450 REV A.SDR FDEA202010212578Frame · crackedNR 2 PYLON AFT FAIRING, OUTBOARD FRAME HAS A CRACKED CLIP. REMOVED AND REPLACED CLIP ON NR 2 PYLON AFT FAIRING, PER B767 SRM 51-40-02 AND BAC DWG 313T3380 REV F.SDR FDEA202010202567Floorbeam · crackedFLOOR BEAM SUPPORT ANGLE CRACKED IN THE E&E BAY LEFT SIDE TUNNEL. REMOVE AND REPLACED FLOOR SUPPORT ANGLE, PER BAC DWG 141T5600 REV E.SDR FDEA202010202566Former · crackedLEFT WING LEADING EDGE NOSE FORMER AT STA OSS 565.90 IS CRACKED. REMOVED AND REPLACED NOSE FORMER PER FEDEX EA H 5720-T0357475 P1 WINGS-SECONDARY WING STRCT-LT WING, LEADING EDGE, ANGLE, OSS 566, ALTERNATE FASTENERS AND BAC DWG 114T2162 REV.SDR FDEA202010202565Angle · crackedNR 1 ENGINE AFT A FRAME AFT INBOARD ANGLE CRACKED. REMOVE AND REPLACED ANGLE 313T3380-69, PER BAC DWG 313T2303 REV.SDR FDEA202010182551Former · crackedLEFT WING LEADING EDGE FORMER CRACKED AT NR 5 SLAT OUTBOARD ROTARY ACTUATOR. REMOVED CRACKED FORMER AND INSTALLED NEW FORMER P/N 114T2511U13, REF BAC DWG 114T2161 REV.SDR FDEA202010162524Seal Depressor · crackedMAIN CARGO DOOR AFT UPPER SEAL DEPRESSOR IS CRACKED AND GOUGED. REMOVED AND REPLACED SEAL DEPRESSOR P/N 143T8194-7, IAW B767 SRM 51-40-02 AND BAC DWG 143T8194 REV.SDR FDEA202004170755Unknown · odorSTRONG SMELL WHILE PULLING INTO GATE. SOURCE UNDETERMINED. ODOR WENT AWAY AFTER SHUTDOWN. SIMILAR TO A SMOLDERING ODOR POSSIBLE. RAN BOTH ENGINES AND PACK AND APU REF 767 JRH JRHFX1, COULD NOT DUPLICATE ODOR OR SMELL, BUMPED ENGINES UP AND TURNED PACKES SDR FDEA2019062751408Escape Rope · unsecureDURING A PREFLIGHT INSPECTION, FOUND THE ENTRY DOOR EMERGENCY ESCAPE ROPE NOT STOWED. STOWED THE ESCAPE ROPE IAW AMM 25-10-00-2. ACFT OK FOR SERVICE.
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